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Development of preliminary design concept for a multifunction display and control system for the Orbiter crew station. Task 4: Design concept recommendationApplication of multifunction display and control systems to the NASA Orbiter spacecraft offers the potential for reducing crew workload and improving the presentation of system status and operational data to the crew. A design concept is presented for the application of a multifunction display and control system (MFDCS) to the Orbital Maneuvering System and Electrical Power Distribution and Control System on the Orbiter spacecraft. The MFDCS would provide the capability for automation of procedures, fault prioritization and software reconfiguration of the MFDCS data base. The MFDCS would operate as a stand-alone processor to minimize the impact on the current Orbiter software. Supervisory crew command of all current functions would be retained through the use of several operating modes in the system. Both the design concept and the processes followed in defining the concept are described.
Document ID
19830004881
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Spiger, R. J.
(Boeing Co. Seattle, WA, United States)
Farrell, R. J.
(Boeing Co. Seattle, WA, United States)
Holcomb, G. A.
(Boeing Co. Seattle, WA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-167769
NAS 1.26:167769
D180-27215-1
Report Number: NASA-CR-167769
Report Number: NAS 1.26:167769
Report Number: D180-27215-1
Accession Number
83N13152
Funding Number(s)
CONTRACT_GRANT: NAS9-16445
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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